501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
16x16 (16x16.dat)
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v2022-0915
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Simulation Date: 09/22/2022
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AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS
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====== PERFORMANCE DATA (versus advance ratio and MPH) ======
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DEFINITIONS:
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J=V/nD (advance ratio)
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Ct=T/(rho * n**2 * D**4) (thrust coef.)
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Cp=P/(rho * n**3 * D**5) (power coef.)
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Pe=Ct*J/Cp (efficiency)
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V (model speed in MPH)
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Mach (at prop tip)
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Reyn (at 75% of span)
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FOM (Figure of Merit)
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PROP RPM = 1000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1213 0.0668 0.006 0.355 0.253 4.201 0.040 1.127 27.364 0.06 30363. 0.5052
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0.60 0.0397 0.0703 0.1209 0.0683 0.006 0.363 0.253 4.295 0.041 1.124 26.675 0.06 30396. 0.4917
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1.20 0.0793 0.1368 0.1205 0.0699 0.006 0.372 0.252 4.398 0.042 1.119 25.953 0.06 30433. 0.4775
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1.80 0.1190 0.1993 0.1200 0.0717 0.006 0.381 0.251 4.510 0.043 1.115 25.203 0.06 30476. 0.4627
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2.40 0.1587 0.2576 0.1194 0.0736 0.006 0.391 0.249 4.628 0.044 1.109 24.433 0.06 30525. 0.4474
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3.01 0.1984 0.3117 0.1186 0.0755 0.006 0.402 0.248 4.751 0.045 1.102 23.652 0.06 30580. 0.4318
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3.61 0.2380 0.3616 0.1177 0.0775 0.007 0.412 0.246 4.877 0.047 1.094 22.866 0.06 30641. 0.4158
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4.21 0.2777 0.4074 0.1166 0.0795 0.007 0.423 0.244 5.002 0.048 1.083 22.084 0.06 30709. 0.3997
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4.81 0.3174 0.4493 0.1152 0.0814 0.007 0.433 0.241 5.122 0.049 1.071 21.312 0.06 30783. 0.3834
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5.41 0.3571 0.4875 0.1136 0.0832 0.007 0.442 0.237 5.234 0.050 1.055 20.554 0.06 30865. 0.3671
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6.01 0.3967 0.5222 0.1115 0.0847 0.007 0.451 0.233 5.332 0.051 1.036 19.814 0.06 30955. 0.3507
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6.61 0.4364 0.5536 0.1091 0.0860 0.007 0.457 0.228 5.410 0.052 1.013 19.095 0.06 31051. 0.3342
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7.21 0.4761 0.5818 0.1061 0.0868 0.007 0.462 0.222 5.463 0.052 0.986 18.398 0.06 31155. 0.3176
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7.81 0.5158 0.6071 0.1026 0.0872 0.007 0.464 0.214 5.484 0.052 0.953 17.722 0.06 31267. 0.3008
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8.42 0.5554 0.6297 0.0985 0.0869 0.007 0.462 0.206 5.466 0.052 0.915 17.067 0.06 31386. 0.2839
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9.02 0.5951 0.6496 0.0938 0.0859 0.007 0.457 0.196 5.407 0.052 0.871 16.432 0.06 31512. 0.2667
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9.62 0.6348 0.6668 0.0886 0.0843 0.007 0.448 0.185 5.306 0.051 0.823 15.813 0.06 31645. 0.2494
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10.22 0.6745 0.6811 0.0829 0.0821 0.007 0.437 0.173 5.165 0.049 0.770 15.203 0.06 31786. 0.2320
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10.82 0.7141 0.6924 0.0769 0.0793 0.007 0.422 0.161 4.988 0.048 0.714 14.597 0.07 31933. 0.2145
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11.42 0.7538 0.7003 0.0705 0.0759 0.006 0.404 0.147 4.777 0.046 0.655 13.986 0.07 32087. 0.1968
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12.02 0.7935 0.7042 0.0640 0.0721 0.006 0.383 0.134 4.534 0.043 0.594 13.360 0.07 32247. 0.1791
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12.62 0.8332 0.7033 0.0572 0.0677 0.006 0.360 0.119 4.263 0.041 0.531 12.708 0.07 32414. 0.1611
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13.22 0.8728 0.6965 0.0503 0.0630 0.005 0.335 0.105 3.963 0.038 0.467 12.013 0.07 32588. 0.1427
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13.83 0.9125 0.6821 0.0432 0.0578 0.005 0.307 0.090 3.636 0.035 0.401 11.254 0.07 32768. 0.1240
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14.43 0.9522 0.6576 0.0361 0.0522 0.004 0.278 0.075 3.285 0.031 0.335 10.397 0.07 32954. 0.1046
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15.03 0.9919 0.6186 0.0288 0.0462 0.004 0.246 0.060 2.909 0.028 0.268 9.389 0.07 33146. 0.0845
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15.63 1.0315 0.5578 0.0216 0.0399 0.003 0.212 0.045 2.510 0.024 0.200 8.140 0.07 33344. 0.0634
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16.23 1.0712 0.4614 0.0143 0.0332 0.003 0.177 0.030 2.092 0.020 0.133 6.484 0.07 33548. 0.0411
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16.83 1.1109 0.3001 0.0071 0.0263 0.002 0.140 0.015 1.655 0.016 0.066 4.066 0.07 33758. 0.0182
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17.43 1.1506 -0.0021 0.0000 0.0191 0.002 0.102 0.000 1.202 0.011 0.000 -0.028 0.07 33971. 0.0000
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PROP RPM = 2000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1218 0.0611 0.041 1.301 1.017 30.779 0.147 4.525 14.993 0.13 60726. 0.5546
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1.23 0.0406 0.0786 0.1214 0.0627 0.042 1.334 1.014 31.564 0.151 4.512 14.575 0.13 60793. 0.5383
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2.46 0.0812 0.1525 0.1210 0.0644 0.043 1.370 1.011 32.427 0.155 4.496 14.138 0.13 60870. 0.5213
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3.69 0.1218 0.2215 0.1205 0.0663 0.045 1.410 1.007 33.361 0.159 4.478 13.687 0.13 60959. 0.5036
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4.92 0.1624 0.2854 0.1199 0.0682 0.046 1.452 1.002 34.355 0.164 4.456 13.225 0.13 61059. 0.4854
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6.15 0.2030 0.3442 0.1192 0.0703 0.047 1.496 0.996 35.393 0.169 4.429 12.759 0.13 61172. 0.4669
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7.38 0.2436 0.3979 0.1183 0.0724 0.049 1.541 0.988 36.454 0.174 4.395 12.294 0.13 61299. 0.4482
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8.61 0.2842 0.4469 0.1171 0.0745 0.050 1.585 0.979 37.510 0.179 4.353 11.834 0.13 61440. 0.4293
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9.84 0.3249 0.4912 0.1157 0.0765 0.052 1.628 0.967 38.527 0.184 4.301 11.383 0.13 61596. 0.4105
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11.07 0.3655 0.5313 0.1140 0.0784 0.053 1.668 0.952 39.468 0.188 4.236 10.944 0.13 61767. 0.3917
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12.31 0.4061 0.5675 0.1119 0.0800 0.054 1.703 0.934 40.290 0.192 4.156 10.520 0.13 61953. 0.3729
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13.54 0.4467 0.6000 0.1093 0.0813 0.055 1.730 0.913 40.944 0.195 4.060 10.111 0.13 62155. 0.3542
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14.77 0.4873 0.6291 0.1061 0.0822 0.055 1.749 0.887 41.374 0.198 3.943 9.719 0.13 62372. 0.3356
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16.00 0.5279 0.6552 0.1024 0.0825 0.056 1.755 0.855 41.521 0.198 3.804 9.343 0.13 62604. 0.3169
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17.23 0.5685 0.6784 0.0980 0.0821 0.055 1.747 0.819 41.336 0.197 3.641 8.983 0.13 62853. 0.2981
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18.46 0.6091 0.6990 0.0930 0.0810 0.055 1.724 0.777 40.796 0.195 3.456 8.639 0.13 63116. 0.2793
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19.69 0.6497 0.7170 0.0875 0.0793 0.054 1.686 0.731 39.905 0.191 3.251 8.308 0.13 63394. 0.2605
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20.92 0.6903 0.7324 0.0815 0.0768 0.052 1.635 0.681 38.683 0.185 3.030 7.986 0.13 63687. 0.2417
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22.15 0.7309 0.7449 0.0752 0.0738 0.050 1.570 0.628 37.154 0.177 2.795 7.672 0.13 63994. 0.2230
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23.38 0.7715 0.7542 0.0686 0.0702 0.047 1.494 0.573 35.340 0.169 2.550 7.359 0.13 64315. 0.2043
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24.61 0.8121 0.7599 0.0618 0.0661 0.045 1.405 0.516 33.257 0.159 2.297 7.043 0.13 64650. 0.1856
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25.84 0.8527 0.7610 0.0548 0.0614 0.041 1.307 0.458 30.921 0.148 2.037 6.718 0.13 64998. 0.1667
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27.07 0.8934 0.7566 0.0477 0.0563 0.038 1.198 0.398 28.342 0.135 1.772 6.375 0.13 65360. 0.1476
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28.30 0.9340 0.7446 0.0404 0.0507 0.034 1.079 0.338 25.532 0.122 1.502 6.001 0.13 65735. 0.1279
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29.53 0.9746 0.7218 0.0331 0.0447 0.030 0.951 0.277 22.501 0.107 1.230 5.575 0.13 66123. 0.1075
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30.76 1.0152 0.6828 0.0257 0.0383 0.026 0.814 0.215 19.262 0.092 0.956 5.063 0.13 66523. 0.0861
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31.99 1.0558 0.6162 0.0184 0.0315 0.021 0.669 0.153 15.833 0.076 0.682 4.393 0.13 66936. 0.0631
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33.22 1.0964 0.4969 0.0110 0.0243 0.016 0.517 0.092 12.232 0.058 0.409 3.411 0.13 67361. 0.0379
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34.45 1.1370 0.2526 0.0037 0.0169 0.011 0.359 0.031 8.484 0.041 0.139 1.673 0.13 67796. 0.0108
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35.68 1.1776
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1220 0.0589 0.134 2.819 2.294 100.057 0.318 10.202 10.398 0.19 91089. 0.5775
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1.82 0.0401 0.0807 0.1217 0.0604 0.138 2.893 2.287 102.686 0.327 10.174 10.103 0.19 91187. 0.5603
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3.64 0.0801 0.1564 0.1213 0.0621 0.142 2.974 2.280 105.576 0.336 10.141 9.795 0.19 91301. 0.5424
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5.46 0.1202 0.2270 0.1208 0.0640 0.146 3.063 2.271 108.706 0.346 10.103 9.477 0.19 91431. 0.5238
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7.28 0.1603 0.2923 0.1203 0.0660 0.150 3.157 2.261 112.045 0.357 10.057 9.153 0.19 91579. 0.5047
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9.11 0.2003 0.3523 0.1196 0.0680 0.155 3.255 2.248 115.542 0.368 10.000 8.826 0.19 91745. 0.4853
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10.93 0.2404 0.4071 0.1188 0.0701 0.160 3.356 2.232 119.127 0.379 9.930 8.500 0.19 91932. 0.4657
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12.75 0.2804 0.4570 0.1177 0.0722 0.165 3.457 2.212 122.714 0.391 9.841 8.178 0.19 92139. 0.4461
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14.57 0.3205 0.5022 0.1164 0.0743 0.169 3.555 2.188 126.197 0.402 9.730 7.862 0.19 92367. 0.4265
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16.39 0.3606 0.5429 0.1147 0.0762 0.174 3.647 2.157 129.451 0.412 9.593 7.556 0.19 92617. 0.4070
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18.21 0.4006 0.5797 0.1127 0.0779 0.177 3.729 2.119 132.341 0.421 9.423 7.261 0.19 92889. 0.3876
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20.03 0.4407 0.6127 0.1102 0.0793 0.181 3.795 2.072 134.708 0.429 9.217 6.977 0.19 93185. 0.3683
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21.85 0.4808 0.6424 0.1073 0.0803 0.183 3.842 2.016 136.374 0.434 8.968 6.706 0.19 93502. 0.3492
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23.67 0.5208 0.6690 0.1037 0.0807 0.184 3.864 1.949 137.144 0.437 8.670 6.446 0.19 93843. 0.3300
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25.50 0.5609 0.6929 0.0995 0.0805 0.184 3.855 1.870 136.842 0.436 8.319 6.199 0.19 94206. 0.3109
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27.32 0.6010 0.7142 0.0947 0.0797 0.182 3.814 1.780 135.373 0.431 7.918 5.964 0.19 94592. 0.2918
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29.14 0.6410 0.7332 0.0894 0.0781 0.178 3.740 1.680 132.729 0.422 7.471 5.740 0.19 94999. 0.2728
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30.96 0.6811 0.7498 0.0836 0.0759 0.173 3.634 1.571 128.966 0.411 6.987 5.524 0.19 95428. 0.2539
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32.78 0.7212 0.7638 0.0774 0.0731 0.166 3.498 1.455 124.157 0.395 6.472 5.315 0.20 95877. 0.2351
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34.60 0.7612 0.7752 0.0710 0.0697 0.159 3.335 1.334 118.373 0.377 5.933 5.111 0.20 96348. 0.2164
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36.42 0.8013 0.7835 0.0643 0.0657 0.150 3.146 1.208 111.672 0.355 5.374 4.907 0.20 96838. 0.1978
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38.24 0.8413 0.7882 0.0574 0.0613 0.140 2.933 1.079 104.103 0.331 4.800 4.701 0.20 97348. 0.1791
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40.06 0.8814 0.7884 0.0504 0.0563 0.128 2.696 0.947 95.706 0.305 4.213 4.489 0.20 97878. 0.1602
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41.89 0.9215 0.7828 0.0433 0.0509 0.116 2.437 0.813 86.515 0.275 3.617 4.263 0.20 98427. 0.1410
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43.71 0.9615 0.7691 0.0360 0.0451 0.103 2.157 0.678 76.566 0.244 3.014 4.014 0.20 98995. 0.1212
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45.53 1.0016 0.7432 0.0288 0.0388 0.088 1.857 0.541 65.899 0.210 2.406 3.724 0.20 99582. 0.1004
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47.35 1.0417 0.6973 0.0215 0.0321 0.073 1.537 0.404 54.564 0.174 1.797 3.359 0.20 100187. 0.0783
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49.17 1.0817 0.6138 0.0142 0.0251 0.057 1.201 0.268 42.623 0.136 1.190 2.847 0.20 100810. 0.0540
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50.99 1.1218 0.4447 0.0070 0.0177 0.040 0.850 0.132 30.154 0.096 0.588 1.989 0.20 101449. 0.0265
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52.81 1.1619 -0.0104 -0.0001 0.0101 0.023 0.484 -0.002 17.176 0.055 -0.008 -0.045 0.20 102085. 0.0000
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1222 0.0577 0.312 4.911 4.084 232.416 0.555 18.168 7.971 0.25 121450. 0.5908
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2.43 0.0401 0.0825 0.1219 0.0593 0.320 5.043 4.074 238.676 0.570 18.119 7.741 0.25 121582. 0.5730
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4.86 0.0802 0.1599 0.1215 0.0610 0.329 5.189 4.061 245.569 0.586 18.064 7.501 0.25 121733. 0.5544
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7.30 0.1204 0.2320 0.1211 0.0628 0.339 5.347 4.047 253.050 0.604 18.000 7.254 0.25 121907. 0.5351
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9.73 0.1605 0.2986 0.1206 0.0648 0.350 5.516 4.029 261.045 0.623 17.923 7.001 0.25 122105. 0.5154
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12.16 0.2006 0.3596 0.1199 0.0669 0.361 5.693 4.008 269.436 0.643 17.827 6.747 0.25 122327. 0.4953
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14.59 0.2407 0.4153 0.1191 0.0690 0.373 5.876 3.981 278.060 0.664 17.706 6.493 0.25 122576. 0.4751
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17.02 0.2809 0.4659 0.1181 0.0712 0.384 6.058 3.946 286.707 0.684 17.553 6.243 0.25 122852. 0.4548
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19.45 0.3210 0.5116 0.1168 0.0733 0.396 6.236 3.903 295.125 0.705 17.361 5.999 0.26 123157. 0.4346
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21.89 0.3611 0.5528 0.1152 0.0752 0.406 6.403 3.849 303.017 0.723 17.121 5.762 0.26 123492. 0.4146
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24.32 0.4012 0.5899 0.1132 0.0770 0.416 6.552 3.783 310.049 0.740 16.825 5.534 0.26 123856. 0.3947
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26.75 0.4414 0.6233 0.1108 0.0784 0.424 6.674 3.701 315.843 0.754 16.462 5.315 0.26 124251. 0.3750
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29.18 0.4815 0.6532 0.1078 0.0795 0.429 6.761 3.602 319.965 0.764 16.021 5.106 0.26 124676. 0.3554
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31.61 0.5216 0.6800 0.1042 0.0799 0.432 6.803 3.483 321.945 0.769 15.491 4.907 0.26 125131. 0.3358
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34.05 0.5617 0.7041 0.1000 0.0798 0.431 6.791 3.343 321.360 0.767 14.868 4.718 0.26 125617. 0.3163
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36.48 0.6019 0.7258 0.0952 0.0790 0.426 6.719 3.182 317.971 0.759 14.152 4.539 0.26 126132. 0.2969
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38.91 0.6420 0.7451 0.0899 0.0774 0.418 6.588 3.002 311.757 0.744 13.355 4.368 0.26 126677. 0.2776
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41.34 0.6821 0.7622 0.0840 0.0752 0.406 6.399 2.808 302.845 0.723 12.490 4.206 0.26 127250. 0.2584
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43.77 0.7222 0.7769 0.0778 0.0724 0.391 6.158 2.601 291.408 0.696 11.570 4.049 0.26 127852. 0.2395
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46.20 0.7624 0.7891 0.0714 0.0689 0.372 5.866 2.384 277.614 0.663 10.606 3.896 0.26 128481. 0.2206
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48.64 0.8025 0.7985 0.0646 0.0650 0.351 5.528 2.160 261.602 0.625 9.607 3.745 0.26 129136. 0.2018
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51.07 0.8426 0.8045 0.0577 0.0605 0.327 5.145 1.929 243.489 0.581 8.581 3.594 0.26 129819. 0.1830
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53.50 0.8827 0.8065 0.0507 0.0555 0.300 4.720 1.693 223.368 0.533 7.532 3.439 0.26 130527. 0.1641
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55.93 0.9229 0.8031 0.0435 0.0500 0.270 4.254 1.454 201.322 0.481 6.467 3.275 0.26 131261. 0.1448
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58.36 0.9630 0.7923 0.0363 0.0441 0.238 3.749 1.211 177.439 0.424 5.388 3.097 0.27 132021. 0.1250
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60.79 1.0031 0.7703 0.0289 0.0377 0.204 3.208 0.967 151.815 0.362 4.303 2.890 0.27 132806. 0.1042
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63.23 1.0432 0.7294 0.0216 0.0309 0.167 2.632 0.723 124.572 0.297 3.215 2.631 0.27 133615. 0.0820
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65.66 1.0834 0.6522 0.0143 0.0238 0.129 2.026 0.479 95.864 0.229 2.130 2.266 0.27 134447. 0.0575
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68.09 1.1235 0.4876 0.0071 0.0164 0.088 1.392 0.237 65.878 0.157 1.055 1.633 0.27 135302. 0.0292
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70.52 1.1636 -0.0090 -0.0001 0.0086 0.046 0.731 -0.002 34.616 0.083 -0.010 -0.029 0.27 136145. 0.0000
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PROP RPM = 5000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1224 0.0571 0.602 7.585 6.392 448.720 0.857 28.433 6.461 0.32 151810. 0.5991
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3.04 0.0402 0.0837 0.1221 0.0586 0.618 7.793 6.376 460.985 0.880 28.361 6.274 0.32 151975. 0.5810
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6.09 0.0804 0.1622 0.1218 0.0603 0.636 8.021 6.358 474.514 0.906 28.281 6.078 0.32 152165. 0.5620
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9.13 0.1206 0.2353 0.1214 0.0622 0.656 8.270 6.337 489.229 0.934 28.188 5.875 0.32 152382. 0.5424
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12.18 0.1608 0.3027 0.1209 0.0642 0.677 8.537 6.312 504.990 0.964 28.074 5.669 0.32 152629. 0.5223
|
|
15.22 0.2009 0.3644 0.1203 0.0663 0.699 8.817 6.280 521.573 0.996 27.932 5.461 0.32 152908. 0.5019
|
|
18.27 0.2411 0.4207 0.1195 0.0685 0.722 9.106 6.239 538.661 1.029 27.752 5.254 0.32 153219. 0.4812
|
|
21.31 0.2813 0.4717 0.1185 0.0707 0.745 9.396 6.188 555.842 1.062 27.523 5.049 0.32 153566. 0.4606
|
|
24.36 0.3215 0.5178 0.1173 0.0728 0.768 9.680 6.122 572.612 1.094 27.233 4.850 0.32 153948. 0.4401
|
|
27.40 0.3617 0.5593 0.1157 0.0748 0.789 9.946 6.040 588.381 1.124 26.867 4.656 0.32 154367. 0.4197
|
|
30.45 0.4019 0.5966 0.1137 0.0766 0.808 10.185 5.938 602.480 1.151 26.412 4.470 0.32 154823. 0.3995
|
|
33.49 0.4421 0.6302 0.1113 0.0781 0.824 10.382 5.812 614.154 1.173 25.851 4.292 0.32 155318. 0.3795
|
|
36.53 0.4823 0.6603 0.1084 0.0791 0.835 10.524 5.658 622.537 1.189 25.167 4.122 0.32 155851. 0.3596
|
|
39.58 0.5224 0.6873 0.1048 0.0797 0.840 10.594 5.473 626.689 1.197 24.342 3.961 0.32 156422. 0.3398
|
|
42.62 0.5626 0.7116 0.1006 0.0796 0.839 10.578 5.254 625.764 1.195 23.368 3.808 0.32 157031. 0.3201
|
|
45.67 0.6028 0.7334 0.0958 0.0787 0.830 10.469 5.002 619.274 1.183 22.247 3.663 0.32 157678. 0.3005
|
|
48.71 0.6430 0.7531 0.0904 0.0772 0.814 10.264 4.720 607.172 1.160 20.997 3.526 0.32 158361. 0.2810
|
|
51.76 0.6832 0.7705 0.0846 0.0750 0.791 9.969 4.415 589.701 1.126 19.637 3.396 0.32 159080. 0.2617
|
|
54.80 0.7234 0.7857 0.0783 0.0721 0.761 9.588 4.090 567.202 1.083 18.191 3.270 0.33 159834. 0.2425
|
|
57.85 0.7636 0.7985 0.0718 0.0687 0.724 9.129 3.749 540.008 1.031 16.674 3.149 0.33 160623. 0.2236
|
|
60.89 0.8038 0.8086 0.0650 0.0646 0.682 8.594 3.395 508.397 0.971 15.103 3.029 0.33 161445. 0.2047
|
|
63.94 0.8439 0.8157 0.0581 0.0601 0.634 7.989 3.032 472.596 0.903 13.487 2.910 0.33 162301. 0.1858
|
|
66.98 0.8841 0.8189 0.0510 0.0550 0.580 7.316 2.661 432.792 0.827 11.836 2.789 0.33 163189. 0.1668
|
|
70.02 0.9243 0.8172 0.0437 0.0495 0.522 6.578 2.284 389.153 0.743 10.159 2.662 0.33 164110. 0.1475
|
|
73.07 0.9645 0.8085 0.0364 0.0435 0.458 5.779 1.902 341.849 0.653 8.461 2.524 0.33 165062. 0.1277
|
|
76.11 1.0047 0.7893 0.0291 0.0370 0.390 4.920 1.518 291.075 0.556 6.752 2.365 0.33 166046. 0.1069
|
|
79.16 1.0449 0.7521 0.0217 0.0301 0.318 4.008 1.133 237.076 0.453 5.039 2.167 0.33 167060. 0.0846
|
|
82.20 1.0851 0.6794 0.0143 0.0229 0.242 3.046 0.749 180.161 0.344 3.331 1.885 0.34 168104. 0.0598
|
|
85.25 1.1253 0.5176 0.0071 0.0153 0.162 2.040 0.369 120.705 0.231 1.639 1.385 0.34 169174. 0.0308
|
|
88.29 1.1654 -0.0271 -0.0002 0.0074 0.079 0.990 -0.009 58.582 0.112 -0.040 -0.070 0.34 170218. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 6000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1226 0.0567 1.033 10.856 9.220 770.641 1.227 41.013 5.427 0.38 182169. 0.6043
|
|
3.68 0.0405 0.0851 0.1223 0.0583 1.062 11.157 9.199 792.023 1.261 40.916 5.268 0.38 182368. 0.5859
|
|
7.37 0.0811 0.1648 0.1220 0.0600 1.094 11.490 9.175 815.677 1.298 40.809 5.102 0.38 182598. 0.5667
|
|
11.05 0.1216 0.2389 0.1216 0.0619 1.128 11.854 9.146 841.477 1.339 40.683 4.930 0.38 182862. 0.5468
|
|
14.74 0.1621 0.3072 0.1212 0.0640 1.166 12.244 9.112 869.191 1.383 40.529 4.755 0.38 183161. 0.5264
|
|
18.42 0.2026 0.3697 0.1206 0.0661 1.205 12.656 9.068 898.432 1.430 40.336 4.578 0.38 183500. 0.5056
|
|
22.11 0.2432 0.4266 0.1199 0.0683 1.245 13.082 9.013 928.639 1.478 40.088 4.402 0.38 183878. 0.4846
|
|
25.79 0.2837 0.4781 0.1189 0.0706 1.286 13.511 8.941 959.073 1.526 39.770 4.228 0.38 184299. 0.4637
|
|
29.47 0.3242 0.5245 0.1177 0.0728 1.326 13.930 8.849 988.823 1.574 39.360 4.059 0.38 184764. 0.4428
|
|
33.16 0.3647 0.5662 0.1161 0.0748 1.364 14.324 8.732 1016.814 1.618 38.840 3.895 0.38 185274. 0.4221
|
|
36.84 0.4053 0.6037 0.1142 0.0767 1.397 14.676 8.585 1041.823 1.658 38.186 3.738 0.38 185831. 0.4016
|
|
40.53 0.4458 0.6373 0.1118 0.0782 1.425 14.967 8.402 1062.463 1.691 37.373 3.587 0.38 186433. 0.3813
|
|
44.21 0.4863 0.6675 0.1088 0.0793 1.444 15.174 8.178 1077.161 1.714 36.376 3.444 0.39 187083. 0.3612
|
|
47.90 0.5269 0.6945 0.1052 0.0798 1.454 15.273 7.907 1084.208 1.726 35.169 3.308 0.39 187779. 0.3411
|
|
51.58 0.5674 0.7189 0.1009 0.0796 1.451 15.244 7.585 1082.107 1.722 33.737 3.179 0.39 188521. 0.3211
|
|
55.26 0.6079 0.7409 0.0960 0.0787 1.435 15.074 7.214 1070.034 1.703 32.089 3.058 0.39 189310. 0.3012
|
|
58.95 0.6484 0.7607 0.0904 0.0771 1.405 14.763 6.800 1047.952 1.668 30.249 2.943 0.39 190143. 0.2815
|
|
62.63 0.6890 0.7783 0.0845 0.0748 1.363 14.317 6.351 1016.323 1.618 28.250 2.834 0.39 191019. 0.2620
|
|
66.32 0.7295 0.7937 0.0781 0.0718 1.309 13.746 5.873 975.769 1.553 26.124 2.730 0.39 191939. 0.2426
|
|
70.00 0.7700 0.8068 0.0715 0.0682 1.243 13.057 5.372 926.880 1.475 23.896 2.629 0.39 192900. 0.2235
|
|
73.69 0.8106 0.8173 0.0646 0.0640 1.167 12.258 4.853 870.144 1.385 21.588 2.530 0.39 193903. 0.2044
|
|
77.37 0.8511 0.8247 0.0575 0.0593 1.081 11.354 4.320 805.962 1.283 19.216 2.431 0.39 194945. 0.1853
|
|
81.06 0.8916 0.8283 0.0502 0.0541 0.985 10.349 3.776 734.664 1.169 16.794 2.331 0.40 196028. 0.1661
|
|
84.74 0.9321 0.8270 0.0429 0.0483 0.880 9.249 3.222 656.552 1.045 14.333 2.226 0.40 197150. 0.1466
|
|
88.42 0.9727 0.8186 0.0354 0.0421 0.767 8.057 2.663 571.936 0.910 11.845 2.112 0.40 198310. 0.1264
|
|
92.11 1.0132 0.7992 0.0279 0.0354 0.645 6.778 2.100 481.182 0.766 9.340 1.979 0.40 199508. 0.1052
|
|
95.79 1.0537 0.7604 0.0204 0.0283 0.516 5.420 1.536 384.749 0.612 6.832 1.811 0.40 200744. 0.0823
|
|
99.48 1.0942 0.6805 0.0130 0.0208 0.380 3.990 0.974 283.224 0.451 4.334 1.560 0.40 202015. 0.0565
|
|
103.16 1.1348 0.4846 0.0056 0.0130 0.238 2.498 0.419 177.290 0.282 1.863 1.072 0.40 203316. 0.0254
|
|
106.85 1.1753
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1229 0.0566 1.637 14.743 12.573 1221.001 1.666 55.924 4.670 0.44 212525. 0.6073
|
|
4.30 0.0406 0.0855 0.1226 0.0581 1.683 15.153 12.546 1254.934 1.712 55.803 4.534 0.44 212758. 0.5890
|
|
8.60 0.0811 0.1657 0.1223 0.0599 1.733 15.607 12.516 1292.568 1.763 55.670 4.392 0.44 213026. 0.5698
|
|
12.91 0.1217 0.2401 0.1220 0.0618 1.789 16.104 12.481 1333.738 1.819 55.514 4.244 0.44 213334. 0.5499
|
|
17.21 0.1622 0.3088 0.1215 0.0639 1.848 16.640 12.438 1378.106 1.880 55.325 4.094 0.44 213684. 0.5295
|
|
21.51 0.2028 0.3717 0.1210 0.0660 1.911 17.207 12.384 1425.083 1.944 55.085 3.942 0.45 214078. 0.5087
|
|
25.81 0.2434 0.4289 0.1203 0.0683 1.976 17.796 12.314 1473.801 2.011 54.774 3.790 0.45 214520. 0.4877
|
|
30.11 0.2839 0.4806 0.1194 0.0706 2.042 18.391 12.223 1523.080 2.078 54.368 3.640 0.45 215011. 0.4667
|
|
34.42 0.3245 0.5271 0.1183 0.0728 2.107 18.975 12.105 1571.451 2.144 53.841 3.494 0.45 215554. 0.4458
|
|
38.72 0.3651 0.5690 0.1168 0.0749 2.169 19.527 11.952 1617.160 2.206 53.163 3.352 0.45 216150. 0.4250
|
|
43.02 0.4056 0.6066 0.1149 0.0768 2.224 20.022 11.758 1658.201 2.262 52.301 3.216 0.45 216800. 0.4045
|
|
47.32 0.4462 0.6403 0.1125 0.0784 2.269 20.434 11.516 1692.306 2.309 51.222 3.086 0.45 217504. 0.3841
|
|
51.62 0.4867 0.6706 0.1096 0.0796 2.302 20.731 11.215 1716.901 2.342 49.886 2.963 0.45 218263. 0.3639
|
|
55.93 0.5273 0.6977 0.1060 0.0801 2.319 20.879 10.850 1729.200 2.359 48.259 2.846 0.45 219077. 0.3438
|
|
60.23 0.5679 0.7223 0.1018 0.0800 2.316 20.850 10.414 1726.735 2.356 46.320 2.735 0.45 219945. 0.3237
|
|
64.53 0.6084 0.7444 0.0968 0.0791 2.291 20.625 9.909 1708.108 2.330 44.077 2.631 0.45 220866. 0.3038
|
|
68.83 0.6490 0.7644 0.0913 0.0775 2.244 20.203 9.345 1673.218 2.283 41.566 2.533 0.45 221840. 0.2840
|
|
73.13 0.6896 0.7823 0.0853 0.0752 2.176 19.595 8.730 1622.798 2.214 38.831 2.440 0.45 222865. 0.2644
|
|
77.44 0.7301 0.7981 0.0789 0.0722 2.089 18.811 8.075 1557.860 2.125 35.918 2.351 0.46 223940. 0.2450
|
|
81.74 0.7707 0.8117 0.0722 0.0685 1.984 17.863 7.388 1479.370 2.018 32.862 2.265 0.46 225064. 0.2258
|
|
86.04 0.8112 0.8227 0.0652 0.0643 1.862 16.761 6.675 1388.138 1.894 29.693 2.181 0.46 226236. 0.2067
|
|
90.34 0.8518 0.8309 0.0581 0.0595 1.723 15.514 5.943 1284.815 1.753 26.433 2.098 0.46 227456. 0.1876
|
|
94.64 0.8924 0.8355 0.0508 0.0542 1.569 14.127 5.194 1169.945 1.596 23.103 2.014 0.46 228721. 0.1683
|
|
98.95 0.9329 0.8354 0.0433 0.0484 1.400 12.606 4.433 1044.017 1.424 19.718 1.926 0.46 230032. 0.1487
|
|
103.25 0.9735 0.8287 0.0358 0.0420 1.217 10.958 3.663 907.539 1.238 16.294 1.831 0.47 231389. 0.1285
|
|
107.55 1.0141 0.8115 0.0282 0.0353 1.021 9.190 2.888 761.098 1.038 12.846 1.721 0.47 232789. 0.1073
|
|
111.85 1.0546 0.7756 0.0206 0.0281 0.812 7.310 2.111 605.442 0.826 9.391 1.582 0.47 234233. 0.0843
|
|
116.15 1.0952 0.7000 0.0131 0.0205 0.592 5.331 1.338 441.527 0.602 5.952 1.375 0.47 235718. 0.0583
|
|
120.46 1.1357 0.5072 0.0056 0.0125 0.363 3.266 0.573 270.465 0.369 2.548 0.960 0.47 237238. 0.0267
|
|
124.76 1.1763
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1231 0.0566 2.446 19.273 16.453 1824.178 2.177 73.185 4.091 0.51 242880. 0.6086
|
|
4.90 0.0404 0.0853 0.1229 0.0582 2.514 19.804 16.421 1874.473 2.237 73.043 3.974 0.51 243144. 0.5905
|
|
9.80 0.0808 0.1654 0.1226 0.0599 2.589 20.395 16.387 1930.387 2.304 72.887 3.850 0.51 243449. 0.5716
|
|
14.70 0.1212 0.2398 0.1223 0.0618 2.671 21.043 16.346 1991.742 2.377 72.709 3.722 0.51 243798. 0.5519
|
|
19.59 0.1616 0.3085 0.1219 0.0639 2.760 21.744 16.298 2058.104 2.457 72.491 3.592 0.51 244195. 0.5317
|
|
24.49 0.2021 0.3714 0.1215 0.0661 2.855 22.490 16.235 2128.677 2.541 72.215 3.459 0.51 244643. 0.5112
|
|
29.39 0.2425 0.4287 0.1209 0.0684 2.953 23.267 16.154 2202.226 2.629 71.853 3.327 0.51 245144. 0.4904
|
|
34.29 0.2829 0.4805 0.1200 0.0707 3.054 24.058 16.046 2277.040 2.718 71.374 3.196 0.51 245702. 0.4696
|
|
39.19 0.3233 0.5271 0.1190 0.0730 3.153 24.838 15.904 2350.926 2.806 70.742 3.068 0.51 246318. 0.4488
|
|
44.09 0.3637 0.5691 0.1176 0.0752 3.247 25.581 15.719 2421.244 2.890 69.917 2.945 0.51 246994. 0.4281
|
|
48.98 0.4041 0.6068 0.1158 0.0771 3.332 26.254 15.480 2484.944 2.966 68.855 2.826 0.51 247731. 0.4077
|
|
53.88 0.4445 0.6406 0.1135 0.0788 3.404 26.821 15.177 2538.569 3.030 67.509 2.712 0.51 248530. 0.3874
|
|
58.78 0.4849 0.6709 0.1107 0.0800 3.457 27.240 14.800 2578.216 3.078 65.829 2.604 0.51 249392. 0.3673
|
|
63.68 0.5254 0.6983 0.1073 0.0807 3.486 27.466 14.336 2599.649 3.103 63.766 2.501 0.51 250316. 0.3473
|
|
68.58 0.5658 0.7229 0.1031 0.0807 3.485 27.459 13.779 2599.009 3.102 61.287 2.405 0.52 251302. 0.3273
|
|
73.48 0.6062 0.7453 0.0982 0.0799 3.452 27.195 13.130 2573.964 3.072 58.402 2.314 0.52 252348. 0.3075
|
|
78.37 0.6466 0.7655 0.0928 0.0784 3.385 26.668 12.399 2524.158 3.013 55.152 2.228 0.52 253455. 0.2877
|
|
83.27 0.6870 0.7838 0.0868 0.0761 3.286 25.891 11.600 2450.613 2.925 51.598 2.147 0.52 254620. 0.2682
|
|
88.17 0.7274 0.8001 0.0804 0.0731 3.158 24.880 10.746 2354.867 2.811 47.798 2.070 0.52 255841. 0.2488
|
|
93.07 0.7678 0.8142 0.0737 0.0695 3.002 23.650 9.848 2238.416 2.672 43.802 1.995 0.52 257118. 0.2296
|
|
97.97 0.8082 0.8259 0.0667 0.0653 2.820 22.214 8.914 2102.526 2.510 39.651 1.923 0.52 258450. 0.2106
|
|
102.87 0.8487 0.8350 0.0595 0.0605 2.613 20.584 7.953 1948.219 2.326 35.376 1.852 0.53 259835. 0.1915
|
|
107.77 0.8891 0.8408 0.0521 0.0551 2.382 18.768 6.970 1776.339 2.120 31.002 1.780 0.53 261272. 0.1723
|
|
112.66 0.9295 0.8423 0.0447 0.0493 2.129 16.774 5.969 1587.632 1.895 26.552 1.705 0.53 262762. 0.1528
|
|
117.56 0.9699 0.8378 0.0371 0.0429 1.854 14.610 4.956 1382.856 1.651 22.046 1.626 0.53 264303. 0.1327
|
|
122.46 1.0103 0.8240 0.0294 0.0361 1.559 12.286 3.935 1162.878 1.388 17.503 1.535 0.53 265893. 0.1117
|
|
127.36 1.0507 0.7937 0.0218 0.0288 1.246 9.813 2.911 928.792 1.109 12.948 1.422 0.54 267533. 0.0889
|
|
132.26 1.0911 0.7288 0.0141 0.0212 0.915 7.206 1.890 682.005 0.814 8.407 1.257 0.54 269220. 0.0634
|
|
137.16 1.1315 0.5649 0.0066 0.0132 0.569 4.482 0.879 424.201 0.506 3.908 0.939 0.54 270948. 0.0323
|
|
142.05 1.1719
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1234 0.0568 3.496 24.480 20.867 2606.692 2.766 92.817 3.631 0.57 273232. 0.6083
|
|
5.49 0.0403 0.0849 0.1231 0.0584 3.591 25.147 20.831 2677.630 2.841 92.656 3.529 0.57 273528. 0.5906
|
|
10.98 0.0805 0.1647 0.1229 0.0601 3.697 25.889 20.793 2756.713 2.925 92.485 3.421 0.57 273869. 0.5721
|
|
16.47 0.1208 0.2389 0.1227 0.0620 3.814 26.707 20.749 2843.789 3.017 92.291 3.309 0.57 274259. 0.5528
|
|
21.96 0.1610 0.3076 0.1223 0.0641 3.940 27.595 20.696 2938.365 3.118 92.057 3.195 0.57 274703. 0.5330
|
|
27.45 0.2013 0.3705 0.1219 0.0663 4.076 28.545 20.629 3039.447 3.225 91.758 3.078 0.57 275202. 0.5128
|
|
32.94 0.2416 0.4277 0.1214 0.0686 4.218 29.540 20.540 3145.406 3.337 91.363 2.962 0.57 275762. 0.4923
|
|
38.43 0.2818 0.4796 0.1207 0.0709 4.364 30.559 20.420 3253.906 3.453 90.830 2.846 0.57 276384. 0.4717
|
|
43.92 0.3221 0.5263 0.1198 0.0733 4.508 31.572 20.259 3361.856 3.567 90.114 2.733 0.57 277072. 0.4512
|
|
49.41 0.3623 0.5683 0.1185 0.0755 4.647 32.545 20.045 3465.447 3.677 89.160 2.624 0.57 277826. 0.4308
|
|
54.90 0.4026 0.6060 0.1168 0.0776 4.774 33.435 19.764 3560.231 3.778 87.911 2.518 0.58 278649. 0.4105
|
|
60.39 0.4429 0.6399 0.1147 0.0794 4.883 34.195 19.403 3641.146 3.863 86.305 2.417 0.58 279542. 0.3904
|
|
65.88 0.4831 0.6703 0.1120 0.0807 4.965 34.772 18.947 3702.500 3.928 84.275 2.321 0.58 280504. 0.3705
|
|
71.37 0.5234 0.6978 0.1086 0.0815 5.013 35.106 18.380 3738.098 3.966 81.754 2.230 0.58 281537. 0.3506
|
|
76.86 0.5636 0.7226 0.1046 0.0816 5.018 35.144 17.693 3742.162 3.971 78.700 2.145 0.58 282639. 0.3308
|
|
82.35 0.6039 0.7451 0.0998 0.0809 4.976 34.851 16.887 3710.965 3.937 75.113 2.064 0.58 283809. 0.3110
|
|
87.84 0.6441 0.7656 0.0944 0.0794 4.886 34.219 15.972 3643.664 3.866 71.044 1.988 0.58 285047. 0.2914
|
|
93.33 0.6844 0.7842 0.0885 0.0772 4.749 33.260 14.966 3541.590 3.758 66.569 1.917 0.58 286349. 0.2719
|
|
98.82 0.7247 0.8009 0.0821 0.0743 4.569 31.996 13.886 3406.958 3.615 61.766 1.849 0.59 287716. 0.2526
|
|
104.31 0.7649 0.8155 0.0754 0.0707 4.348 30.447 12.747 3242.011 3.440 56.700 1.783 0.59 289144. 0.2335
|
|
109.80 0.8052 0.8279 0.0683 0.0665 4.088 28.631 11.561 3048.669 3.235 51.425 1.720 0.59 290633. 0.2145
|
|
115.29 0.8454 0.8379 0.0611 0.0617 3.793 26.563 10.338 2828.463 3.001 45.982 1.658 0.59 292182. 0.1955
|
|
120.78 0.8857 0.8447 0.0537 0.0563 3.463 24.255 9.084 2582.660 2.740 40.407 1.595 0.59 293790. 0.1763
|
|
126.27 0.9260 0.8477 0.0462 0.0504 3.101 21.716 7.807 2312.354 2.453 34.727 1.531 0.60 295456. 0.1569
|
|
131.76 0.9662 0.8452 0.0385 0.0440 2.707 18.958 6.513 2018.636 2.142 28.968 1.463 0.60 297178. 0.1369
|
|
137.25 1.0065 0.8344 0.0308 0.0371 2.283 15.991 5.206 1702.726 1.807 23.156 1.387 0.60 298956. 0.1160
|
|
142.74 1.0467 0.8090 0.0230 0.0298 1.832 12.830 3.894 1366.154 1.450 17.321 1.293 0.60 300789. 0.0936
|
|
148.23 1.0870 0.7536 0.0153 0.0220 1.356 9.494 2.585 1010.888 1.073 11.496 1.160 0.60 302675. 0.0684
|
|
153.72 1.1273 0.6146 0.0076 0.0139 0.857 6.004 1.285 639.355 0.678 5.718 0.912 0.61 304609. 0.0379
|
|
159.21 1.1675 -0.0137 -0.0001 0.0054 0.334 2.341 -0.011 249.309 0.265 -0.048 -0.020 0.61 306441. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1236 0.0573 4.832 30.454 25.819 3603.106 3.441 114.842 3.250 0.63 303581. 0.6056
|
|
6.10 0.0403 0.0846 0.1234 0.0588 4.961 31.268 25.779 3699.361 3.533 114.665 3.161 0.63 303910. 0.5885
|
|
12.21 0.0806 0.1641 0.1232 0.0605 5.105 32.178 25.738 3807.063 3.635 114.484 3.066 0.63 304288. 0.5705
|
|
18.31 0.1209 0.2383 0.1230 0.0624 5.265 33.185 25.693 3926.149 3.749 114.283 2.968 0.64 304722. 0.5518
|
|
24.42 0.1611 0.3069 0.1228 0.0645 5.439 34.283 25.640 4056.122 3.873 114.045 2.867 0.64 305214. 0.5324
|
|
30.52 0.2014 0.3699 0.1224 0.0667 5.627 35.464 25.571 4195.813 4.007 113.741 2.764 0.64 305769. 0.5126
|
|
36.62 0.2417 0.4272 0.1220 0.0690 5.824 36.710 25.479 4343.189 4.147 113.332 2.661 0.64 306390. 0.4926
|
|
42.73 0.2820 0.4792 0.1214 0.0714 6.028 37.994 25.353 4495.191 4.293 112.769 2.558 0.64 307081. 0.4724
|
|
48.83 0.3223 0.5260 0.1206 0.0739 6.233 39.283 25.178 4647.610 4.438 111.991 2.457 0.64 307844. 0.4522
|
|
54.94 0.3626 0.5681 0.1194 0.0762 6.430 40.529 24.939 4795.104 4.579 110.928 2.359 0.64 308682. 0.4320
|
|
61.04 0.4029 0.6059 0.1179 0.0784 6.613 41.681 24.619 4931.312 4.709 109.503 2.264 0.64 309597. 0.4120
|
|
67.15 0.4432 0.6399 0.1159 0.0802 6.771 42.675 24.198 5048.924 4.821 107.633 2.174 0.64 310589. 0.3922
|
|
73.25 0.4834 0.6704 0.1133 0.0817 6.892 43.442 23.657 5139.727 4.908 105.228 2.088 0.64 311660. 0.3724
|
|
79.35 0.5237 0.6979 0.1100 0.0826 6.966 43.907 22.977 5194.742 4.961 102.202 2.006 0.64 312809. 0.3527
|
|
85.46 0.5640 0.7228 0.1060 0.0827 6.981 43.998 22.143 5205.496 4.971 98.492 1.929 0.64 314035. 0.3329
|
|
91.56 0.6043 0.7455 0.1013 0.0821 6.928 43.667 21.155 5166.324 4.933 94.096 1.857 0.65 315339. 0.3133
|
|
97.67 0.6446 0.7662 0.0959 0.0807 6.807 42.901 20.026 5075.751 4.847 89.075 1.790 0.65 316717. 0.2937
|
|
103.77 0.6849 0.7850 0.0899 0.0784 6.619 41.716 18.778 4935.553 4.713 83.524 1.726 0.65 318168. 0.2742
|
|
109.87 0.7252 0.8020 0.0835 0.0755 6.368 40.139 17.433 4748.914 4.535 77.542 1.665 0.65 319690. 0.2550
|
|
115.98 0.7655 0.8171 0.0767 0.0718 6.060 38.197 16.011 4519.129 4.315 71.218 1.607 0.65 321281. 0.2358
|
|
122.08 0.8057 0.8300 0.0696 0.0675 5.698 35.914 14.528 4249.003 4.057 64.620 1.551 0.66 322939. 0.2168
|
|
128.19 0.8460 0.8405 0.0622 0.0626 5.285 33.308 12.995 3940.788 3.763 57.802 1.496 0.66 324664. 0.1977
|
|
134.29 0.8863 0.8481 0.0547 0.0572 4.823 30.397 11.423 3596.314 3.434 50.808 1.441 0.66 326454. 0.1786
|
|
140.39 0.9266 0.8520 0.0470 0.0511 4.314 27.192 9.819 3217.168 3.072 43.675 1.384 0.66 328309. 0.1591
|
|
146.50 0.9669 0.8508 0.0392 0.0446 3.761 23.708 8.192 2804.888 2.678 36.437 1.325 0.66 330226. 0.1390
|
|
152.60 1.0072 0.8415 0.0314 0.0375 3.166 19.957 6.548 2361.198 2.255 29.126 1.258 0.67 332206. 0.1180
|
|
158.71 1.0475 0.8183 0.0234 0.0300 2.532 15.960 4.896 1888.240 1.803 21.778 1.176 0.67 334246. 0.0954
|
|
164.81 1.0878 0.7659 0.0155 0.0221 1.862 11.739 3.246 1388.818 1.326 14.438 1.060 0.67 336345. 0.0700
|
|
170.92 1.1280 0.6306 0.0077 0.0138 1.162 7.324 1.608 866.493 0.827 7.151 0.842 0.67 338496. 0.0391
|
|
177.02 1.1683 -0.0357 -0.0002 0.0050 0.425 2.680 -0.032 317.062 0.303 -0.143 -0.046 0.68 340495. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 11000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1239 0.0585 6.566 37.620 31.308 4895.968 4.250 139.260 2.900 0.70 333927. 0.5952
|
|
6.72 0.0403 0.0832 0.1237 0.0600 6.734 38.582 31.266 5021.226 4.359 139.070 2.824 0.70 334288. 0.5791
|
|
13.43 0.0806 0.1616 0.1236 0.0616 6.922 39.663 31.224 5161.917 4.481 138.883 2.744 0.70 334704. 0.5622
|
|
20.15 0.1209 0.2349 0.1234 0.0635 7.132 40.864 31.180 5318.125 4.617 138.687 2.659 0.70 335181. 0.5445
|
|
26.87 0.1612 0.3029 0.1232 0.0655 7.361 42.180 31.129 5489.400 4.765 138.460 2.572 0.70 335721. 0.5263
|
|
33.58 0.2015 0.3656 0.1229 0.0678 7.610 43.602 31.064 5674.452 4.926 138.173 2.483 0.70 336331. 0.5075
|
|
40.30 0.2418 0.4228 0.1226 0.0701 7.873 45.111 30.976 5870.835 5.097 137.782 2.393 0.70 337013. 0.4885
|
|
47.02 0.2821 0.4748 0.1221 0.0725 8.146 46.677 30.852 6074.677 5.274 137.230 2.304 0.70 337771. 0.4692
|
|
53.73 0.3224 0.5218 0.1214 0.0750 8.422 48.258 30.675 6280.457 5.452 136.442 2.215 0.70 338609. 0.4500
|
|
60.45 0.3627 0.5643 0.1204 0.0774 8.691 49.799 30.425 6480.927 5.626 135.329 2.129 0.70 339529. 0.4307
|
|
67.16 0.4030 0.6025 0.1190 0.0796 8.941 51.231 30.078 6667.319 5.788 133.789 2.046 0.70 340534. 0.4115
|
|
73.88 0.4433 0.6369 0.1172 0.0815 9.159 52.477 29.611 6829.547 5.929 131.709 1.967 0.71 341624. 0.3924
|
|
80.60 0.4836 0.6680 0.1147 0.0831 9.329 53.452 28.995 6956.349 6.039 128.971 1.891 0.71 342802. 0.3733
|
|
87.31 0.5239 0.6960 0.1116 0.0840 9.435 54.060 28.206 7035.472 6.108 125.458 1.818 0.71 344067. 0.3542
|
|
94.03 0.5642 0.7214 0.1077 0.0842 9.461 54.211 27.222 7055.153 6.125 121.086 1.750 0.71 345418. 0.3349
|
|
100.75 0.6045 0.7445 0.1031 0.0837 9.397 53.842 26.043 7007.150 6.083 115.839 1.686 0.71 346853. 0.3155
|
|
107.46 0.6448 0.7656 0.0977 0.0823 9.238 52.933 24.683 6888.832 5.980 109.788 1.625 0.71 348372. 0.2961
|
|
114.18 0.6851 0.7848 0.0917 0.0800 8.988 51.499 23.168 6702.183 5.818 103.051 1.568 0.71 349971. 0.2768
|
|
120.90 0.7254 0.8022 0.0852 0.0770 8.651 49.571 21.528 6451.325 5.601 95.755 1.514 0.72 351648. 0.2575
|
|
127.61 0.7657 0.8177 0.0783 0.0733 8.235 47.184 19.787 6140.659 5.331 88.012 1.462 0.72 353402. 0.2384
|
|
134.33 0.8060 0.8311 0.0711 0.0689 7.743 44.367 17.966 5774.090 5.013 79.914 1.411 0.72 355230. 0.2194
|
|
141.05 0.8463 0.8423 0.0636 0.0639 7.181 41.146 16.081 5354.844 4.649 71.530 1.362 0.72 357131. 0.2003
|
|
147.76 0.8866 0.8507 0.0560 0.0583 6.552 37.539 14.145 4885.501 4.241 62.915 1.313 0.73 359103. 0.1811
|
|
154.48 0.9269 0.8555 0.0481 0.0522 5.858 33.565 12.167 4368.311 3.792 54.117 1.263 0.73 361146. 0.1616
|
|
161.19 0.9672 0.8554 0.0402 0.0454 5.103 29.241 10.156 3805.508 3.304 45.176 1.211 0.73 363258. 0.1415
|
|
167.91 1.0075 0.8477 0.0321 0.0382 4.291 24.586 8.124 3199.677 2.778 36.134 1.152 0.73 365438. 0.1204
|
|
174.63 1.0478 0.8263 0.0241 0.0305 3.425 19.626 6.078 2554.161 2.217 27.036 1.079 0.74 367685. 0.0976
|
|
181.34 1.0881 0.7760 0.0160 0.0224 2.512 14.396 4.032 1873.563 1.626 17.934 0.976 0.74 369996. 0.0719
|
|
188.06 1.1284 0.6417 0.0079 0.0139 1.561 8.944 1.997 1163.952 1.010 8.884 0.778 0.74 372363. 0.0403
|
|
194.78 1.1687 -0.0417 -0.0002 0.0050 0.564 3.232 -0.045 420.669 0.365 -0.202 -0.049 0.74 374540. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1241 0.0614 8.954 47.027 37.327 6676.641 5.313 166.030 2.536 0.76 364269. 0.5681
|
|
7.33 0.0403 0.0795 0.1240 0.0629 9.165 48.137 37.280 6834.153 5.438 165.822 2.474 0.76 364662. 0.5540
|
|
14.65 0.0806 0.1547 0.1238 0.0645 9.403 49.388 37.236 7011.849 5.580 165.628 2.409 0.76 365116. 0.5390
|
|
21.98 0.1209 0.2254 0.1237 0.0663 9.669 50.784 37.193 7210.021 5.738 165.436 2.340 0.76 365634. 0.5233
|
|
29.31 0.1612 0.2914 0.1235 0.0683 9.962 52.322 37.147 7428.354 5.911 165.229 2.268 0.76 366223. 0.5070
|
|
36.63 0.2015 0.3524 0.1233 0.0705 10.280 53.992 37.090 7665.460 6.100 164.976 2.195 0.76 366886. 0.4902
|
|
43.96 0.2418 0.4086 0.1231 0.0728 10.619 55.774 37.013 7918.478 6.301 164.633 2.120 0.76 367629. 0.4730
|
|
51.28 0.2821 0.4599 0.1227 0.0753 10.973 57.634 36.901 8182.564 6.511 164.136 2.045 0.76 368453. 0.4557
|
|
58.61 0.3224 0.5066 0.1221 0.0777 11.332 59.521 36.736 8450.473 6.725 163.402 1.972 0.77 369364. 0.4383
|
|
65.94 0.3627 0.5492 0.1213 0.0801 11.683 61.365 36.493 8712.280 6.933 162.320 1.900 0.77 370365. 0.4209
|
|
73.26 0.4029 0.5879 0.1202 0.0824 12.010 63.079 36.142 8955.559 7.127 160.761 1.830 0.77 371458. 0.4036
|
|
80.59 0.4432 0.6233 0.1185 0.0843 12.292 64.561 35.651 9165.973 7.294 158.575 1.764 0.77 372646. 0.3863
|
|
87.92 0.4835 0.6556 0.1163 0.0858 12.509 65.702 34.983 9328.023 7.423 155.602 1.701 0.77 373929. 0.3690
|
|
95.24 0.5238 0.6852 0.1134 0.0867 12.640 66.389 34.102 9425.561 7.501 151.685 1.641 0.77 375307. 0.3514
|
|
102.57 0.5641 0.7123 0.1097 0.0869 12.664 66.515 32.982 9443.395 7.515 146.702 1.584 0.77 376781. 0.3336
|
|
109.90 0.6044 0.7372 0.1051 0.0862 12.567 66.004 31.614 9370.921 7.457 140.618 1.530 0.78 378348. 0.3155
|
|
117.22 0.6447 0.7600 0.0998 0.0847 12.344 64.836 30.014 9205.064 7.325 133.503 1.479 0.78 380007. 0.2971
|
|
124.55 0.6850 0.7808 0.0938 0.0823 12.001 63.033 28.215 8949.071 7.121 125.500 1.430 0.78 381754. 0.2786
|
|
131.87 0.7253 0.7996 0.0873 0.0792 11.545 60.638 26.252 8609.037 6.851 116.768 1.383 0.78 383587. 0.2599
|
|
139.20 0.7656 0.8163 0.0803 0.0753 10.985 57.695 24.157 8191.156 6.518 107.452 1.338 0.78 385503. 0.2411
|
|
146.53 0.8059 0.8308 0.0730 0.0708 10.326 54.238 21.958 7700.461 6.128 97.670 1.293 0.79 387500. 0.2223
|
|
153.85 0.8462 0.8429 0.0654 0.0657 9.576 50.297 19.675 7140.899 5.683 87.513 1.250 0.79 389577. 0.2033
|
|
161.18 0.8865 0.8521 0.0576 0.0599 8.737 45.892 17.323 6515.434 5.185 77.052 1.206 0.79 391732. 0.1841
|
|
168.51 0.9268 0.8577 0.0496 0.0536 7.814 41.041 14.916 5826.798 4.637 66.345 1.161 0.79 393963. 0.1644
|
|
175.83 0.9671 0.8582 0.0414 0.0467 6.810 35.770 12.465 5078.355 4.041 55.445 1.113 0.80 396269. 0.1441
|
|
183.16 1.0074 0.8504 0.0332 0.0393 5.733 30.110 9.982 4274.891 3.402 44.400 1.059 0.80 398649. 0.1227
|
|
190.49 1.0477 0.8275 0.0249 0.0315 4.590 24.110 7.478 3423.033 2.724 33.263 0.991 0.80 401101. 0.0994
|
|
197.81 1.0880 0.7717 0.0165 0.0233 3.395 17.833 4.967 2531.757 2.015 22.093 0.890 0.81 403623. 0.0727
|
|
205.14 1.1283 0.6231 0.0082 0.0148 2.162 11.358 2.463 1612.565 1.283 10.957 0.693 0.81 406206. 0.0399
|
|
212.46 1.1686 -0.0336 -0.0002 0.0061 0.891 4.682 -0.053 664.785 0.529 -0.235 -0.036 0.81 408609. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1242 0.0674 12.487 60.543 43.850 9311.826 6.840 195.045 2.136 0.83 394605. 0.5187
|
|
7.94 0.0403 0.0728 0.1241 0.0688 12.746 61.796 43.794 9504.562 6.982 194.797 2.090 0.83 395031. 0.5072
|
|
15.88 0.0806 0.1421 0.1239 0.0703 13.039 63.219 43.745 9723.365 7.142 194.577 2.041 0.83 395522. 0.4950
|
|
23.83 0.1210 0.2077 0.1238 0.0721 13.368 64.815 43.700 9968.862 7.323 194.376 1.988 0.83 396084. 0.4820
|
|
31.77 0.1613 0.2693 0.1237 0.0741 13.733 66.584 43.655 10241.021 7.523 194.177 1.933 0.83 396722. 0.4685
|
|
39.71 0.2016 0.3267 0.1235 0.0762 14.132 68.519 43.605 10538.586 7.741 193.954 1.877 0.83 397440. 0.4545
|
|
47.65 0.2419 0.3799 0.1234 0.0785 14.561 70.598 43.540 10858.399 7.976 193.666 1.819 0.83 398243. 0.4401
|
|
55.59 0.2823 0.4290 0.1231 0.0810 15.012 72.785 43.446 11194.732 8.223 193.249 1.760 0.83 399135. 0.4255
|
|
63.54 0.3226 0.4742 0.1227 0.0835 15.473 75.019 43.304 11538.383 8.476 192.616 1.702 0.83 400120. 0.4108
|
|
71.48 0.3629 0.5157 0.1221 0.0859 15.926 77.214 43.086 11875.875 8.724 191.645 1.646 0.83 401201. 0.3961
|
|
79.42 0.4032 0.5540 0.1211 0.0882 16.346 79.250 42.756 12189.132 8.954 190.178 1.591 0.83 402382. 0.3815
|
|
87.36 0.4435 0.5895 0.1198 0.0901 16.704 80.986 42.272 12456.124 9.150 188.024 1.539 0.83 403666. 0.3670
|
|
95.31 0.4839 0.6228 0.1178 0.0915 16.968 82.264 41.584 12652.707 9.294 184.965 1.491 0.83 405055. 0.3525
|
|
103.25 0.5242 0.6542 0.1152 0.0923 17.106 82.933 40.644 12755.587 9.370 180.783 1.445 0.84 406548. 0.3379
|
|
111.19 0.5645 0.6837 0.1117 0.0922 17.091 82.864 39.411 12744.887 9.362 175.302 1.403 0.84 408146. 0.3229
|
|
119.13 0.6048 0.7115 0.1073 0.0912 16.908 81.976 37.871 12608.342 9.262 168.451 1.362 0.84 409847. 0.3075
|
|
127.07 0.6451 0.7377 0.1021 0.0893 16.554 80.258 36.037 12344.064 9.067 160.291 1.324 0.84 411648. 0.2915
|
|
135.02 0.6855 0.7620 0.0962 0.0865 16.038 77.757 33.944 11959.448 8.785 150.985 1.287 0.84 413547. 0.2751
|
|
142.96 0.7258 0.7844 0.0896 0.0829 15.376 74.547 31.638 11465.758 8.422 140.727 1.252 0.85 415539. 0.2582
|
|
150.90 0.7661 0.8046 0.0826 0.0787 14.582 70.699 29.159 10873.922 7.988 129.699 1.216 0.85 417622. 0.2409
|
|
158.84 0.8064 0.8224 0.0752 0.0737 13.669 66.270 26.541 10192.678 7.487 118.055 1.181 0.85 419793. 0.2231
|
|
166.78 0.8468 0.8375 0.0675 0.0682 12.644 61.303 23.811 9428.792 6.926 105.913 1.145 0.85 422050. 0.2050
|
|
174.73 0.8871 0.8489 0.0595 0.0621 11.520 55.854 20.990 8590.605 6.310 93.363 1.108 0.86 424391. 0.1862
|
|
182.67 0.9274 0.8556 0.0513 0.0556 10.301 49.941 18.093 7681.143 5.642 80.479 1.068 0.86 426815. 0.1667
|
|
190.61 0.9677 0.8548 0.0429 0.0485 8.999 43.630 15.134 6710.514 4.929 67.318 1.023 0.86 429320. 0.1459
|
|
198.55 1.0080 0.8421 0.0344 0.0411 7.625 36.968 12.127 5685.933 4.177 53.942 0.967 0.87 431905. 0.1235
|
|
206.50 1.0484 0.8086 0.0257 0.0334 6.189 30.005 9.088 4614.993 3.390 40.423 0.893 0.87 434567. 0.0987
|
|
214.44 1.0887 0.7320 0.0171 0.0254 4.714 22.853 6.034 3514.949 2.582 26.839 0.779 0.87 437304. 0.0701
|
|
222.38 1.1290 0.5489 0.0085 0.0174 3.227 15.644 2.987 2406.086 1.767 13.285 0.563 0.88 440110. 0.0357
|
|
230.32 1.1693 -0.0202 -0.0002 0.0094 1.738 8.428 -0.057 1296.270 0.952 -0.255 -0.020 0.88 442818. 0.0000
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